NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Development of hydrogen resistant alloysThe most hostile operating environments in the O2/H2 Space Shuttle Main Engine are gaseous hydrogen and hydrogen/water vapor. After years of evaluating commercially available alloys, only a few high strength alloys have been found that perform satisfactorily in these environments. This paper describes the evaluation of various compositions of the Fe-Ni-Co system with elemental additions of Cr, Cb, Ti and Al. After processing, notched tensile specimens were tested in 5000 psi hydrogen at room temperature as the prime screening test. The H2/air ratio was used as the selection/rejection criteria.
Document ID
19850018562
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcpherson, W. B.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: Advan. High Pressure O2(H2 Technol.
Subject Category
Metallic Materials
Accession Number
85N26873
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available